TY - JOUR
T1 - Mechanical System Performance Analysis of Commuter Aircraft's Rear Landing Gear Design for Unpaved Runway
AU - Rammon, N. A.
AU - Nirbito, W.
N1 - Funding Information:
The authors would like to thank PITTA grant program of the University of Indonesia for funding this study with contract number NKB-0796/UN2.R3.1-HKP.05.00/2019, and also to PT. Dirgantara Indonesia (Indonesian Aerospace) high appreciation for the facility, opportunity, and guidance for the development of this study.
Publisher Copyright:
© Published under licence by IOP Publishing Ltd.
PY - 2019/11/22
Y1 - 2019/11/22
N2 - Landing gear design of this commuter aircraft was developed from the previous model, to carry more passengers. The total load of the aircraft will increase as passenger capacity increases. With a variety of runways in Indonesia, it is necessary to have a good landing gear performance for landing on a paved and unpaved runway. Performance of the landing gear design is analyzed through kinematics and dynamics methods. Main concern of this analysis is to find the capability of the landing gear shock absorber to damp the vibration response due to the impact of the landing gear system with the wavy surface of the unpaved runway, as well as the actuator ability as the extension and retraction mechanism driver. The analysis concluded that the landing gear design capable to perform during landing on a paved and unpaved runway, with a modification of the shock absorber and actuator design.
AB - Landing gear design of this commuter aircraft was developed from the previous model, to carry more passengers. The total load of the aircraft will increase as passenger capacity increases. With a variety of runways in Indonesia, it is necessary to have a good landing gear performance for landing on a paved and unpaved runway. Performance of the landing gear design is analyzed through kinematics and dynamics methods. Main concern of this analysis is to find the capability of the landing gear shock absorber to damp the vibration response due to the impact of the landing gear system with the wavy surface of the unpaved runway, as well as the actuator ability as the extension and retraction mechanism driver. The analysis concluded that the landing gear design capable to perform during landing on a paved and unpaved runway, with a modification of the shock absorber and actuator design.
UR - http://www.scopus.com/inward/record.url?scp=85078261074&partnerID=8YFLogxK
U2 - 10.1088/1757-899X/685/1/012006
DO - 10.1088/1757-899X/685/1/012006
M3 - Conference article
AN - SCOPUS:85078261074
VL - 685
JO - IOP Conference Series: Materials Science and Engineering
JF - IOP Conference Series: Materials Science and Engineering
SN - 1757-8981
IS - 1
M1 - 012006
T2 - 3rd International Conference on Aerospace Technology, Communications and Energy Systems, ATCES 2019
Y2 - 26 September 2019 through 29 September 2019
ER -